Problem 1: When a deep space probe is launched, corrections may be necessary to place the probe on a precisely calculated trajectory. Radio telemetry provides a stream of vectors, x1,…,xk, giving information at different times about how the probe’s position compares with its planned trajectory. Let Xk be the matrix [x1…xk]. The matrix Gk=XkXkT is computed as the radar data are analyzed. When xk+1 arrives, a new Gk+1 must be computed. Since the data vectors arrive at high speed, the computational burden could be severe. But partitioned matrix multiplication helps tremendously. Compute the column-row expansions of Gk and Gk+1, and describe what must be computed in order to update Gk to form Gk+1.
Solution: By the column-row expansion rule,
Gk=XkXkT=x1x1T+…+xkxkT.
Similarly,
Gk+1=XkXkT=x1x1T+…+xk+1xk+1T.
Therefore Gk+1=Gk+xk+1xk+1T.
Problem 2: Solve the equation Ax=b by using the LU factorization for A=2−40−68−4406=1−20011001200−6−4048−2 and b=2−46.
Solution: Given the LU factorization of A=LU, it is enough to solve Ly=b and Ux=y consecutively. By row reduction, we have
1−200110012−46∼100011001206∼100010001206.
Therefore y=206. Again by row reduction, we have
200−6−4048−2206∼100−3102−2110−3∼100−3100017−6−3∼100010001−11−6−3.
So the solution of the original equation is x=−11−6−3.